3. Federal Aviation
Administration
Principles of Flight / V.1.07
2
On an End-of-Lesson Test you will identify:
1. Primary and secondary sources of lift.
2. Relative wind.
3. Types and parts of airfoils.
4. Four forces that affect aircraft in flight, their interrelationships,
and the effects on aircraft performance.
5. Effects of altitude, temperature, and pressure on aircraft
performance.
6. Functions of primary and secondary flight controls and the
movement around the aircraft axes.
7. Helicopter aerodynamics.
8. Helicopter controls.
9. Hazards affecting flight.
Objectives
8. Federal Aviation
Administration
Principles of Flight / V.1.07
7
Response Item
• The primary source of lift on an airfoil is
created by a differential in ________.
A. temperature
B. pressure
C. reaction
9. Federal Aviation
Administration
Principles of Flight / V.1.07
8
Response Item
• The statement, “the internal pressure of a
fluid decreases at points where the speed
of the fluid increases” is a part of
________.
A. Bernoulli’s Principle
B. Newton’s Law of Motion
C. Hindenberg’s Theory
13. Federal Aviation
Administration
Principles of Flight / V.1.07
12
Angle of Attack
FLIGHT PATH
20°
5°
10°
The angle of attack is based on the Relative Wind, not the ground.
RELATIVE WIND
RELATIVE WIND
FLIGHT PATH
RELATIVE WIND
FLIGHT PATH
16. Federal Aviation
Administration
Principles of Flight / V.1.07
15
Wing Planforms
Tapered leading edge
and trailing edge
Straight leading
and trailing edges
Delta wing
Straight leading edge,
tapered trailing edge
Tapered leading edge,
straight trailing edge
Sweptback
wings